Table 520.5-VIII: Test Parameter Selection/Profile Development · MIL-STD-810H

Procedure			Step	Task
I	II	III	Step	Task
X	X	X	Step 1	Identify the platform(s), the test materiel installation location(s), and geographical deployment location(s).
X		X	Step 2	Identify the platform(s)/materiel specification requirements. Specification requirements should encompass all planned mission requirements.
	X		Step 2a	Identify the specific mission scenario(s).
X		X	Step 3	Identify applicable individual forcing functions (temperature, altitude, humidity, input electrical power, functional vibration , etc.) (Exception: short term and transient events, e.g., gunfire, crash shock, etc.)
	X		Step 3a	Identify the specific mission forcing functions that support the mission profile. (including climatic, dynamic, and electrical functions)
X	X	X	Step 4	Identify operational requirements of the equipment, including duty cycle, transients, and operational modes (to include all anticipated mission operational scenarios)
X	X	X	Step 5	Identify the temperature, altitude, humidity, input electrical power, and functional vibration levels for each segment of the test profile. See para 2.2.4 and sub paragraphs.
X	X	X	Step 6	Identify the type of cooling (RAM/ECS/convective) and cooling environment for the test item for each segment (see paragraph 2.2.4.1 and 2.2.4.1.1).
X	X	X	Step 7	Develop a table listing all the applicable forcing functions/levels and operational requirements identified in the above steps for each mission or platform.
X		X	Step 8	Identify the applicable combinations of climatic/dynamic/ power parameters considering the full range of platform requirements, as derived from the LCEP. This should include all anticipated combinations of thermal/altitude/humidity/vibration environment and the associated operational/power requirements for each segment of the test profile. For high performance aircraft the Mach/altitude effects shall be considered.
	X		Step 8a	Identify the thermal/altitude/humidity/vibration environment combinations and the associated operational/power requirements for each mission segment (start, idle, taxi, take off, climb, cruise, loiter, combat, maneuver, descent landing).
X		X	Step 9	Using the data identified in steps 1 through 8, develop a representative composite table/profile for thermal, altitude, humidity, functional vibration, test item cooling, and operational power for the most severe expected environments. (see Table 520.5-IX and Figures 520.5-3a and 520.3b)
	X		Step 9a	Using the data identified in steps 1 through 8, develop a thermal, altitude, humidity, functional vibration, test item cooling and operational power profile.

Procedure	Step	Task
X	X	X	Step 1	Identify the platform(s), the test materiel installation location(s), and geographical deployment location(s).
X		X	Step 2	Identify the platform(s)/materiel specification requirements. Specification requirements should encompass all planned mission requirements.
	X		Step 2a	Identify the specific mission scenario(s).
X		X	Step 3	Identify applicable individual forcing functions (temperature, altitude, humidity, input electrical power, functional vibration , etc.) (Exception: short term and transient events, e.g., gunfire, crash shock, etc.)
	X		Step 3a	Identify the specific mission forcing functions that support the mission profile. (including climatic, dynamic, and electrical functions)
X	X	X	Step 4	Identify operational requirements of the equipment, including duty cycle, transients, and operational modes (to include all anticipated mission operational scenarios)
X	X	X	Step 5	Identify the temperature, altitude, humidity, input electrical power, and functional vibration levels for each segment of the test profile. See para 2.2.4 and sub paragraphs.
X	X	X	Step 6	Identify the type of cooling (RAM/ECS/convective) and cooling environment for the test item for each segment (see paragraph 2.2.4.1 and 2.2.4.1.1).
X	X	X	Step 7	Develop a table listing all the applicable forcing functions/levels and operational requirements identified in the above steps for each mission or platform.
X		X	Step 8	Identify the applicable combinations of climatic/dynamic/ power parameters considering the full range of platform requirements, as derived from the LCEP. This should include all anticipated combinations of thermal/altitude/humidity/vibration environment and the associated operational/power requirements for each segment of the test profile. For high performance aircraft the Mach/altitude effects shall be considered.
	X		Step 8a	Identify the thermal/altitude/humidity/vibration environment combinations and the associated operational/power requirements for each mission segment (start, idle, taxi, take off, climb, cruise, loiter, combat, maneuver, descent landing).
X		X	Step 9	Using the data identified in steps 1 through 8, develop a representative composite table/profile for thermal, altitude, humidity, functional vibration, test item cooling, and operational power for the most severe expected environments. (see Table 520.5-IX and Figures 520.5-3a and 520.3b)
	X		Step 9a	Using the data identified in steps 1 through 8, develop a thermal, altitude, humidity, functional vibration, test item cooling and operational power profile.

Procedure

Step

Task

III

Step 1

Identify the platform(s), the test materiel installation location(s), and geographical deployment location(s).

Step 2

Identify the platform(s)/materiel specification requirements. Specification requirements should encompass all planned mission requirements.

Step 2a

Identify the specific mission scenario(s).

Step 3

Identify applicable individual forcing functions (temperature, altitude, humidity, input electrical power, functional vibration , etc.) (Exception: short term and transient events, e.g., gunfire, crash shock, etc.)

Step 3a

Identify the specific mission forcing functions that support the mission profile. (including climatic, dynamic, and electrical functions)

Step 4

Identify operational requirements of the equipment, including duty cycle, transients, and operational modes (to include all anticipated mission operational scenarios)

Step 5

Identify the temperature, altitude, humidity, input electrical power, and functional vibration levels for each segment of the test profile. See para 2.2.4 and sub paragraphs.

Step 6

Identify the type of cooling (RAM/ECS/convective) and cooling environment for the test item for each segment (see paragraph 2.2.4.1 and 2.2.4.1.1).

Step 7

Develop a table listing all the applicable forcing functions/levels and operational requirements identified in the above steps for each mission or platform.

Step 8

Identify the applicable combinations of climatic/dynamic/ power parameters considering the full range of platform requirements, as derived from the LCEP. This should include all anticipated combinations of thermal/altitude/humidity/vibration environment and the associated operational/power requirements for each segment of the test profile. For high performance aircraft the Mach/altitude effects shall be considered.

Step 8a

Identify the thermal/altitude/humidity/vibration environment combinations and the associated operational/power requirements for each mission segment (start, idle, taxi, take off, climb, cruise, loiter, combat, maneuver, descent landing).

Step 9

Using the data identified in steps 1 through 8, develop a representative composite table/profile for thermal, altitude, humidity, functional vibration, test item cooling, and operational power for the most severe expected environments. (see Table 520.5-IX and Figures 520.5-3a and 520.3b)

Step 9a

Using the data identified in steps 1 through 8, develop a thermal, altitude, humidity, functional vibration, test item cooling and operational power profile.